Snecma

Snecma Moteurs

Jean-Luc Goga

Eric Lefebvre

Hervé Buisson

Pierre Lamothe

A fan rotor for an airplane turbojet including locking blade roots in the respective grooves of an airplane turbojet fan rotor. Each blade root is housed in a groove that is closed by a main latch and by an additional latch that is distinct from the main latch and that is spaced apart therefrom by a predetermined distance.

Fan rotor for an airplane turbojet

A rotary assembly comprising a disk having recesses at its periphery; a plurality of blades carried by the disk, each blade having a blade root engaged in a corresponding recess of the disk, and a plurality of fitted platforms each mounted on the disk between two adjacent blades, each platform being a piece of sheet metal of substantially omega section having two flanks interconnected by a web and shaped so as to press against the side walls of the bottom portions of two adjacent blades, with the end portions of the flanks presenting respective setbacks which fit closely to the outlines of one side of a blade root and of the adjacent side of the wall of a recess in which the blade root is received.

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Champagne sur Seine, France

Jean-Luc Goga